Theor. Comput. Fluid Dyn. (2021) 35:757–758 https://doi.org/10.1007/s00162-021-00585-9
C O R R E C T I O N
Hugh J. A. Bird
·Kiran Ramesh
Correction to: Unsteady lifting-line theory and the influence of wake vorticity on aerodynamic loads
Published online: 3 September 2021
© Springer-Verlag GmbH Germany, part of Springer Nature 2021
Correction to: Theor. Comput. Fluid Dyn.
https://doi.org/10.1007/s00162-021-00578-8
The Original publication of this article was published with distorted Figure 7. The correct Fig.
7is given below.
The original article has been corrected.
The original article can be found online athttps://doi.org/10.1007/s00162-021-00578-8 H. J. A. Bird·K. Ramesh (
B
)Aerospace Sciences Division, School of Engineering, University of Glasgow, Glasgow G12 8QQ, UK E-mail: kiran.ramesh@glasgow.ac.uk
H. J. A. Bird
E-mail: hugh.bird.1@research.gla.ac.uk
758 H. J. A. Bird and K. Ramesh
Fig. 7 Comparison of wake vortex sheet strength for an aspect ratio 4 wing oscillating atk=0.5. The ULLT results show only the wake model assumed in the outer domain. Since the wing is shrunk to a line in the outer domain of the ULLTs, thexcoordinate of the trailing edge,xte, is zero for ULLTs. Shown attmod 2π/ω=0
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